Numerical solution of flow equations : an aircraft designer's view
- Today the most accurate and cost effective industrial codes used in aircraft design are based on the full potential equation coupled with boundary layer equations. However, these are not capable to solve complicated three-dimensional problems of vortical flows and shocks. On the other hand Euler and Navier-Stokes codes are too expensive and not accurate enough for design purposes, especially in regard of drag and interference prediction. The reasons for these deficiencies are investigated and a way to overcome them by future developments is demonstrated.
| Author: | Josef Mertens, K. Becker |
|---|---|
| DOI: | https://doi.org/10.1007/978-3-322-87869-4_41 |
| ISBN: | 3-528-08098-1 |
| Parent Title (English): | Nonlinear hyperbolic equations - theory, computation methods, and applications : proceedings of the 2nd International Conference on Nonlinear Hyperbolic Problems, Aachen, FRG, March 14 to 18, 1988. - (Notes on Numerical Fluid Mechanics ; 24) |
| Publisher: | Vieweg |
| Place of publication: | Braunschweig |
| Editor: | Josef Ballmann |
| Document Type: | Part of a Book |
| Language: | English |
| Year of Completion: | 1989 |
| Date of the Publication (Server): | 2012/12/18 |
| Length: | X, 718 S. : zahlr. graph. Darst. |
| First Page: | 403 |
| Last Page: | 412 |
| Note: | International Conference on Nonlinear Hyperbolic Problems <3, 1988, Aachen> |
| Institutes: | FH Aachen / Fachbereich Luft- und Raumfahrttechnik |
| collections: | Verlag / Springer Vieweg |
